Care should be taken to give an appropriate number of significant figures in the final answers to calculations.

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X069/70 NATIONAL QUALIFICATIONS 008 FRIDAY, 3 MAY.00 PM 3.30 PM PHYSICS ADVANCED HIGHER Reference may be made to the Physics Data Booklet. Answer all questions. Any necessary data may be found in the Data Sheet on page three. Care should be taken to give an appropriate number of significant figures in the final answers to calculations. Square-ruled paper (if used) should be placed inside the front cover of the answer book for return to the Scottish Qualifications Authority. LI X069/70 6/4570 *X069/70*

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DATA SHEET COMMON PHYSICAL QUANTITIES Quantity Symbol Value Quantity Symbol Value Gravitational acceleration on Earth g 9. 8m s Mass of electron m e 9. 0 3 kg Radius of Earth R E 6. 4 0 6 m Charge on electron e. 60 0 9 C Mass of Earth M E 6. 0 0 4 kg Mass of neutron m n. 675 0 7 kg Mass of Moon M M 7. 3 0 kg Mass of proton m p. 673 0 7 kg Radius of Moon R M. 7 0 6 m Mass of alpha particle m α 6. 645 0 7 kg Mean Radius of Charge on alpha Moon Orbit 3. 84 0 8 m particle 3. 0 0 9 C Universal constant Planck s constant h 6. 63 0 34 Js of gravitation G 6. 67 0 m 3 kg s Permittivity of free Speed of light in space ε 0 8. 85 0 F m vacuum c 3. 0 0 8 m s Permeability of free Speed of sound in space μ 0 4π 0 7 H m air v 3. 4 0 m s REFRACTIVE INDICES The refractive indices refer to sodium light of wavelength 589 nm and to substances at a temperature of 73 K. Substance Refractive index Substance Refractive index Diamond Glass Ice Perspex. 4. 5. 3. 49 Glycerol Water Air Magnesium Fluoride. 47. 33. 00. 38 SPECTRAL LINES Element Wavelength/nm Colour Element Wavelength/nm Colour Hydrogen Sodium 656 486 434 40 397 389 589 Red Blue-green Blue-violet Violet Ultraviolet Ultraviolet Yellow Cadmium 644 509 480 Lasers Red Green Blue Element Wavelength/nm Colour Carbon dioxide Helium-neon 9550 0590 633 } Infrared Red PROPERTIES OF SELECTED MATERIALS Substance Density/ kg m 3 Melting Point/ K Boiling Point/ K Specific Heat Capacity/ J kg K Specific Latent Heat of Fusion/ J kg Specific Latent Heat of Vaporisation/ J kg Aluminium Copper Glass Ice Glycerol Methanol Sea Water Water Air Hydrogen Nitrogen Oxygen. 70 0 3 8. 96 0 3. 60 0 3 9. 0 0. 6 0 3 7. 9 0. 0 0 3. 00 0 3. 9 9. 0 0. 5. 43 933 357 400 73 9 75 64 73 4 63 55 63 853 563 338 377 373 0 77 90 9. 0 0 3. 86 0 6. 70 0. 0 0 3. 43 0 3. 5 0 3 3. 93 0 3 4. 9 0 3. 43 0 4. 04 0 3 9. 8 0 3. 95 0 5. 05 0 5 3. 34 0 5. 8 0 5 9. 9 0 4 3. 34 0 5 8. 30 0 5. 0 6. 6 0 6 4. 50 0 5. 00 0 5. 40 0 5 The gas densities refer to a temperature of 73 K and a pressure of. 0 0 5 Pa. Page three [Turn over

. A centrifuge is used to separate out small particles suspended in a liquid. Figure shows the rotating part of the centrifuge which includes two test tubes containing the liquid. liquid in test tube Figure The rotating part starts from rest and reaches a maximum angular velocity of 00 rad s in a time of 4 seconds. The average moment of inertia of the rotating part is 5. 0 4 kg m. (a) (i) Calculate the angular acceleration of the rotating part. (ii) Calculate the average unbalanced torque applied during this time. (iii) How many revolutions are made during this time? 3 (b) Figure shows an overhead view of the rotating part. particle 85 mm Figure The expanded view shows the position of a single particle of mass 5. 3 0 6 kg. (i) Calculate the central force acting on the particle at the maximum angular velocity. (ii) What provides the central force acting on this particle? Page four

. (continued) (c) At rest the test tubes in the centrifuge are in a vertical position as shown in Figure 3. Figure 3 Does the moment of inertia of the rotating part increase, decrease, or stay the same during the acceleration of the rotating part? Justify your answer. () [Turn over Page five

. (a) The gravitational field strength g on the surface of Mars is 3. 7Nkg. The mass of Mars is 6. 4 0 3 kg. Show that the radius of Mars is 3. 4 0 6 m. (b) (i) A satellite of mass m has an orbit of radius R. Show that the angular velocity ω of the satellite is given by the expression ω = GM 3 R where the symbols have their usual meanings. (ii) A satellite remains above the same point on the equator of Mars as the planet spins on its axis. Figure 4 shows this satellite orbiting at a height of. 7 0 7 m above the Martian surface.. 7 0 7 m satellite not to scale Figure 4 Calculate the angular velocity of the satellite. (iii) Calculate the length of one Martian day. (c) The following table gives data about three planets orbiting the Sun. Planet Radius R of orbit around the Sun/0 9 m Orbit period T around the Sun/years Venus 08 0. 6 Mars 7. 88 Jupiter 780. 0 Use all the data to show that T is directly proportional to R 3 for these three planets. 3 () Page six

3. A simple pendulum consists of a lead ball on the end of a long string as shown in Figure 5. The ball moves with simple harmonic motion. At time t the displacement s of the ball is given by the expression s = 0 0 cos4 3t s Figure 5 where s is in metres and t in seconds. (a) (i) State the definition of simple harmonic motion. (ii) Calculate the period of the pendulum. (b) Calculate the maximum speed of the ball. (c) The mass of the ball is 5. 0 0 kg and the string has negligible mass. Calculate the total energy of the pendulum. (d) The period T of a pendulum is given by the expression T = π L g (e) where L is the length of the pendulum. Calculate the length of this pendulum. In the above case, the assumption has been made that the motion is not subject to damping. State what is meant by damping. (0) [Turn over Page seven

4. (a) Electrons can exhibit wave-like behaviour. Give one example of evidence which supports this statement. (b) The Bohr model of the hydrogen atom suggests a nucleus with an electron occupying one of a series of stable orbits. A nucleus and the first two stable orbits are shown in Figure 6. nucleus electron Figure 6 not to scale (i) Calculate the angular momentum of the electron in the second stable orbit. (ii) Starting with the relationship mrv = nh π show that the circumference of the second stable orbit is equal to two electron wavelengths. (iii) The circumference of the second stable orbit is. 3 0 9 m. Calculate the speed of the electron in this orbit. (7) Page eight

5. (a) Two point charges Q and Q each has a charge of 4. 0 μc. The charges are 0. 60 m apart as shown in Figure 7. 4. 0 μc 4. 0 μc Q X Q 0. 30 m 0. 30 m Figure 7 (i) Draw a diagram to show the electric field lines between charges Q and Q. (ii) Calculate the electrostatic potential at point X, midway between the charges. (b) A third point charge Q 3 is placed near the two charges as shown in Figure 8. 8. 0 μc Q 3 0. 40 m 4. 0 μc 4. 0 μc Q 0. 60 m Q Figure 8 (i) Show that the force between charges Q and Q 3 is. N. (ii) Calculate the magnitude and direction of the resultant force on charge Q 3 due to charges Q and Q. (7) [Turn over Page nine

6. A student investigates the relationship between the force exerted on a wire in a magnetic field and the current in the wire. A pair of magnets is fixed to a yoke and placed on a top pan Newton balance. A rigid copper wire is suspended between the poles of the magnets. The wire is fixed at 90 to the magnetic field, as shown in Figure 9. s A + d.c. supply S top pan Newton balance Figure 9 With switch S open the balance is set to zero. Switch S is closed. The resistor is adjusted and the force recorded for several values of current. The results are given in the table below. Current/A 0. 50. 00. 50. 00. 50 Force/0 3 N 0. 64 0. 85. 56 3. 07 3. 87 The uncertainty in the current is ± 0. 0 A. The uncertainty in the force is ± 0. 03 0 3 N. Figure 0, on Page eleven, shows the corresponding graph with the best fit straight line for the results. (a) (i) Show that the gradient of the line is. 7 0 3 NA. (ii) Calculate the absolute uncertainty in the gradient of the line. (iii) The length of wire in the magnetic field is 5 mm. Use the information obtained from the graph to calculate the magnitude of the magnetic induction. The uncertainty in the magnetic induction is not required. (b) In the student s evaluation it is stated that the line does not pass through the origin. (i) Suggest a possible reason for this. (ii) Suggest one improvement to the experiment to reduce the absolute uncertainty in the gradient of the line. 3 (8) Page ten

6. (continued) 4. 50 4. 00 3. 50 3. 00 Force/0 3 N. 50. 00. 50. 00 0. 50 0. 00 0. 00 0. 50. 00. 50. 00. 50 3. 00 Current/A Figure 0 [Turn over Page eleven

7. An inductor of negligible resistance is connected in the circuit shown in Figure. S + V A 5 Ω 0. 80 H Figure (a) The inductor has an inductance of 0. 80 H. Switch S is closed. (i) Explain why there is a time delay before the current reaches its maximum value. (ii) Calculate the maximum current in the circuit. (iii) Calculate the maximum energy stored in the inductor. (iv) Calculate the rate of change of current when the current in the circuit is 0. A. 3 (b) Switch S is opened and the iron core is removed from the inductor. Switch S is now closed. (i) Will the maximum current be bigger, smaller or the same as the maximum current calculated in (a)(ii)? (ii) Explain any change in the time delay to reach the maximum current. (iii) Explain why the maximum energy stored in the inductor is less than in (a)(iii). (c) The iron core is replaced in the inductor. The d.c. supply is replaced with a variable frequency supply as shown in Figure. S V ~ A 5 Ω 0. 80 H Figure Sketch a graph to show how the current in the circuit varies with the frequency of the supply. Numerical values are not required. Page twelve (3)

8. (a) Two protons are separated by a distance of μm. (i) (ii) Show by calculation that the gravitational force between these protons is negligible compared to the electrostatic force. Why is the strong force negligible between these protons? 4 (b) A particle of charge q travels directly towards a fixed stationary particle of charge Q. At a large distance from charge Q the moving particle has an initial velocity v. The moving particle momentarily comes to rest at a distance of closest approach r c as shown in Figure 3. +Q +q v +q r c Figure 3 Show that the initial velocity of the moving particle is given by v = qq πε mr 0 c (c) where the symbols have their usual meaning. An alpha particle is fired towards a target nucleus which is fixed and stationary. The initial velocity of the alpha particle is 9. 63 0 6 ms and the distance of closest approach is. 0 3 m. (i) Calculate the charge on the target nucleus. (ii) Calculate the number of protons in the target nucleus. (iii) The target is the nucleus of an element. Identify this element. 3 (3) [Turn over Page thirteen

9. (a) The driver of a sports car approaches a building where an alarm is sounding as shown in Figure 4. alarm Figure 4 The speed of the car is 5. 0ms and the frequency of the sound emitted by the alarm is 50 Hz. (i) Explain in terms of wavefronts why the sound heard by the driver does not have a frequency of 50 Hz. You may wish to include a diagram to support your answer. (ii) Calculate the frequency of the sound from the alarm heard by the driver. Page fourteen

9. (continued) (b) The spectrum of light from most stars contains lines corresponding to helium gas. Figure 5(a) shows the helium spectrum from the Sun. Figure 5(b) shows the helium spectrum from a distant star. 400 500 600 700 wavelength/nm Figure 5(a) 400 500 600 700 wavelength/nm Figure 5(b) By comparing these spectra, what conclusion can be made about the distant star? Justify your answer. (6) [Turn over Page fifteen

0. (a) (i) State what is meant by the term plane polarised light. (ii) Figure 6 shows the refraction of red light at a water-air interface. water air water air 34. 0 34. 0 48. 0 48. 0 red light red light Figure 6 The refractive index n for red light travelling from air to water is. 33. Show that the refractive index μ for red light travelling from water to air is 0. 75. (iii) Figure 7 shows a ray of unpolarised red light incident on a water-air interface. water air Unpolarised red light i p 90 r Polarised light Figure 7 For light travelling from water to air, μ = tan i p where i p is the Brewster angle. Calculate the Brewster angle for red light at this water-air interface. Page sixteen

0. (continued) (b) A rainbow is produced when light follows the path in a raindrop as shown in Figure 8. sunlight raindrop red light violet light Figure 8 The light emerging from the raindrop is polarised. The refractive index, μ, at a water to air interface is 0. 75 for red light and 0. 745 for violet light. Calculate the difference in Brewster s angle for these two colours. (c) Rainbows produce light that is 96% polarised. A photographer plans to take a photograph of a rainbow. Her camera has a polarising filter in front of the lens as shown in Figure 9. Figure 9 She directs her camera at the rainbow and slowly rotates the filter to see which is the best image to take. Describe what happens to the image of the rainbow as she slowly rotates her filter through 80. (7) Page seventeen [Turn over

. Light from a helium-neon laser is incident on a double slit. A pattern of light and dark fringes is observed on a screen 3. 50 m beyond the slits as shown in Figure 0. screen double slit laser 3. 50 m Figure 0 (a) State whether these fringes are caused by division of amplitude or division of wavefront. (b) The distance between two adjacent bright fringes on the screen is 7. 0 mm. Calculate the separation of the two slits. (c) The distance between the double slit and screen is increased to 5. 50 m. The distance between the fringes is remeasured and the calculation of the slit separation is repeated. (i) Explain one advantage of moving the screen further away from the double slit. (ii) State one disadvantage of moving the screen further away from the double slit. (6) [END OF QUESTION PAPER] Page eighteen

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